23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5885230256243036---------------------------
|
|
|
|
Spacecraft: mySat
|
|
dry_mass: 200.0 kg
|
|
specific impulse: 3200.0 kg/s
|
|
max_thrust: 0.00025 kN
|
|
num_thrusters: 1
|
|
duty_cycle: 1.0
|
|
Launch Mass: 3500.0 kg
|
|
Launch Date: 2023-04-23T23:36:39.542
|
|
Launch V∞: [5.4091048971290325, -8.282590969507776, -0.6255449435324507] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.00014378701822437702, 6.294780148211312e-5, -0.0001143721107105596] km/s
|
|
V∞_out: [-4.476106496964864e-5, 0.000148217297878191, 0.00011722583059952925] km/s
|
|
time of flight: 1.4168809102950296e8 seconds
|
|
arrival date: 2027-10-19T21:24:50.542
|
|
thrust profile: [0.28401907544873073 -0.17257200332475836 -0.14181944028908064; 0.18792140754967596 -0.01457482488937606 -0.21147975256250678; 0.13443089839344366 0.01647063571085265 -0.2334268582092854; 0.09602689958411072 0.022675507679729427 -0.2206825610180166; 0.071906508838992 0.02244574412842954 -0.20154271479513863; 0.04093916314469986 0.014462538374285733 -0.13173828063849394; 0.04092574693162532 0.016854228630554653 -0.15059646991754827; 0.016519914172355588 0.00793333603168905 -0.06338110700009074; 0.009748154953515846 0.0047279806894455 -0.04056029248701161; 0.007354597770878847 -0.01528087215524838 -0.02918014035112078; 0.011603430766262166 0.007856208046630052 -0.05210487473933107; 0.005443736085037319 0.0016114769325810204 -0.011260584634345004; 3.206362068602735e-5 0.00696174799996511 -0.014552496409168912; 0.0008814437027630214 -0.0015926866890717047 -0.0007501052905642556; -0.01071236580684505 -0.018017885723490577 0.0002303189226686847; 0.007470193230944855 0.007393746849426102 -0.004583280281227701; -0.01515661116614821 -0.027326755771587007 0.008686480877564247; 0.02889954516824374 -0.017464265584072852 0.028442999036586716; 7.424303492133735e-5 0.004700637077320282 0.0012886034573628127; 0.0012254343244031706 0.0008994950156763605 0.0037475116243666567] %
|
|
|
|
Mass Used: 113.4791565376272 kg
|
|
Launch C3: 98.25103543269606 km²/s²
|
|
||V∞_in||: 0.00019421151363829424 km/s
|